Side-Power SEP 100/185 T Manual de servicio Pagina 20
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Pilot´s Operating Handbook
EXTRA 330LX
Section 2
Limitations
2.4.2 ENGINE LIMITATIONS
a) Maximum Rotational Speed
Take-Off and Maximum Continuous: 2700 rpm*
N O T E*
Applicable RPM limitations approved for the MTV-9-B-C/C 198-25 propeller must be
observed. Refer to Section 2.5.
b) Oil-temperature
- Maximum 118°C (245°F)
c) Oil capacity
- Maximum sump capacity: 15.13 L (16 US.qt)
- Minimum sump capacity: 8.51 L ( 9 US.qt)
d) Oil pressure
- Minimum Idling 172 kPa (25 psig)
- Normal 379 - 655 kPa (55 - 95 psig)
- Starting,Warm up, Taxi and Take-Off 793 kPa (115 psig)
CAUTION
It is normal for the oil pressure to "flicker" from 69 to 207 kPa (10 to 30 psig) when
going from upright to inverted flight. During knife edge flights and zero-g flights oil
pressure may drop and the oil system may not scavenge resulting in engine failure
or damage if flight is prolonged. Knife edge and zero-g flight should not exceed 10
seconds.
WARNING
If oil pressure drops to 0 kPa (psig) the propeller pitch changes automatically to
coarse (high) pitch with a corresponding decrease in RPM. Apply positive g to avoid
engine stoppage.
e) Fuel pressure
at fuel flow divider:
- Maximum 97 kPa (14 psig)
f) Cylinder head temperature
- Max 241°C (465°F)
- EXTRA 330LX 1
- Page Date: 4. February 2011 i 3
- Page Date: 29. September 2014 4
- Page Date: 4. February 2011 v 7
- Left blank intentionally 10
- Section 1 11
- 1.11 CONVERSION TABLE 16
- Section 2 19
- Limitations 19
- TC-NUMBER: * 24
- AVGAS 100/100LL 25
- NO SMOKING 26
- THROTTLE OPEN 27
- MIXTURE RICH 27
- NO HANDHOLD 28
- Section 3 33
- Emergency Procedures 33
- Section 4 43
- Normal Procedures 43
- Section 5 55
- Performance 55
- 5.2 ISA CONVERSION 59
- 5.3 AIRSPEED CALIBRATION 60
- 5.6 RATE OF CLIMB PERFORMANCE 63
- 5.8 RANGE 65
- 5.9 ENDURANCE 66
- Section 6 69
- PILOT COPILOT 76
- REAR SEAT FRONT SEAT 76
- EXAMPLE: 77
- 6.6 EQUIPMENT LIST 78
- EXTRA 330LX S/N: 78
- Reserved 80
- Section 7 87
- Figure 1, Instrument Panel 92
- Figure 3, Fuel System 97
- Figure 4, Electrical System 99
- Section 8 101
- Pilot´s Operating Handbook 101
- Section 9 107
- Supplements 107
- Section 901 109
- Steerable Tail Wheel 109
- Section 902 113
- Electric Pedal Adjustment 113
- Section 903 117
- Cabin Heating System 117
- Section 904 121
- Accelerometer TL-3424_EXT 121
- Section 905 127
- External Power 127
- Section 907 137
- Smoke System 137
- Section 908 145
- Single Seat Canopy 145
- Page Date: 4. Februar 2011 145
- Section 909 149
- ARTEX ME-406 ELT 149
- Section 910 157
- NAT AA83-001 Intercom 157
- HEADSET ONLY 159
- Section 911 165
- BECKER ATC 4401 Transponder 165
- Section 912 173
- BECKER BXP 6401 Transponder 173
- Section 913 183
- GARMIN GTX 327 Transponder 183
- GARMIN GTX 327Transponder 186
- 8 and 9 keys 187
- Section 914 189
- GARMIN GTX 328 Transponder 189
- Section 915 197
- GARMIN GTX 330 Transponder 197
- Section 916 205
- GARMIN GNC 420W/GNS 430W 205
- GARMIN GPS 208
- Section 917 215
- ASPEN EFD1000/500 System 215
- Section 918 225
- EI MVP-50P 225
- Section 919 233
- Landing Light 233
- No change 236
- Section 920 237
- Airtow Hook 237
- TAKE-OFF DISTANCE 242
- Not affected 249
- Section 922 251
- GARMIN GTN 635/650/750 251
- Section 923 267
- EXTRA 300LC 267
- 923.1.2 OPERATION 270
- CONTROLS 270
- Section 924 277
- KANNAD AF 406 ELT 277
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